CN210167746U - Aviation plug wire harness fixing mechanism and aviation plug fixing assembly - Google Patents
Aviation plug wire harness fixing mechanism and aviation plug fixing assembly Download PDFInfo
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- CN210167746U CN210167746U CN201921175142.6U CN201921175142U CN210167746U CN 210167746 U CN210167746 U CN 210167746U CN 201921175142 U CN201921175142 U CN 201921175142U CN 210167746 U CN210167746 U CN 210167746U
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- 230000014759 maintenance of location Effects 0.000 claims description 6
- 238000000034 method Methods 0.000 description 2
- 239000011435 rock Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 238000004873 anchoring Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000014509 gene expression Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
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- 238000012986 modification Methods 0.000 description 1
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Abstract
The utility model discloses an aviation plug wire harness fixing mechanism and an aviation plug fixing assembly, the aviation plug wire harness fixing mechanism comprises a main support, a first support and a closed support; the main support is provided with a plurality of wire harness slots, the wire harness slots extend along the width direction of the main support, each wire harness slot is provided with an opening end and a closed end, and a first support fixing part is arranged on a baffle plate between every two adjacent wire harness slots; the first support bracket comprises a first support section and a first connecting section, an included angle is formed between the first support section and the first connecting section, and the first support section is used for supporting the aviation plug wiring harness; the closing bracket is configured for removable connection with the main bracket to close the open end after the aircraft plug wiring harness enters the harness slot from the open end. The utility model discloses an aviation plug pencil fixed establishment can be spacing at the pencil slot with the aviation plug pencil to support through first support holder, thereby can effectively avoid not hard up of aviation plug.
Description
Technical Field
The utility model relates to a fixed field of aviation plug, more specifically relates to an aviation plug pencil fixed establishment and aviation plug fixed subassembly.
Background
And the display screen of the central control room is electrically connected by adopting an aviation plug. The connection and disconnection of the circuit are realized by the insertion and the separation of the aviation plug and the socket. The connection between the aviation plug and the socket is usually a threaded connection.
For a central control room display screen needing multiple rows of aviation plugs to realize electric connection, wire harnesses for fixing multiple rows of aviation plugs are adopted. The fixing mode easily causes the looseness of the aviation plug due to the clamping of the wiring harness and/or the vibration of the wiring harness, and directly influences the normal use of the display screen of the central control room.
Therefore, how to provide a mechanism capable of stably and effectively fixing the aviation plug wiring harness becomes a technical problem to be solved in the field.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a can stably fix aviation plug pencil fixed establishment's of aviation plug pencil new technical scheme effectively.
According to the utility model discloses a first aspect provides an aviation plug pencil fixed establishment.
The aviation plug wire harness fixing mechanism comprises a main bracket, a first supporting bracket and a closed bracket; wherein,
the wire harness support is characterized in that a plurality of wire harness slots are formed in the main support, the wire harness slots extend along the width direction of the main support, each wire harness slot is provided with an opening end and a closed end, and a first support fixing part is arranged on a baffle plate between every two adjacent wire harness slots;
the first support bracket comprises a first support section and a first connecting section, an included angle is formed between the first support section and the first connecting section, the first support section is used for supporting the aviation plug wiring harness, and the first connecting section is used for being connected with the first support bracket fixing part;
the closing bracket is configured for detachable connection with the main bracket to close the open end after an aircraft plug harness enters the harness slot from the open end.
Optionally, a plurality of the harness slots are arranged in parallel.
Optionally, the depth of the wire harness slot is greater than or equal to 80% of the width of the main bracket.
Optionally, the main bracket has a plate-like shape, and the wire harness slot coverage area is less than or equal to 40% of the surface area of the main bracket.
Optionally, the first support bracket fixing portion is provided with a first support bracket fixing hole.
Optionally, the first supporting section and the first connecting section have a 90 ° included angle therebetween.
Optionally, a plurality of wire binding holes are formed in the first support section.
Optionally, the closing bracket is bolted to the main bracket.
Optionally, the aviation plug wire harness fixing mechanism further comprises a second support bracket;
the second supports the support and includes second support section and second linkage segment, the second support section with have between the second linkage segment and be greater than or equal to 90 contained angle, the second linkage segment with the main support is equipped with one side fixed connection of pencil slot the blind end, the second support section set up to with aviation plug pencil fixed establishment's the plane of placing contacts to support aviation plug pencil fixed establishment on placing the plane.
According to the utility model discloses a second aspect provides a subassembly is fixed to aviation plug.
The aviation plug fixing component comprises an aviation plug, a socket and the aviation plug wire harness fixing mechanism of the utility model; wherein,
the distance between the main bracket and the socket is greater than or equal to 150mm and less than or equal to 300 mm.
The utility model discloses an aviation plug pencil fixed establishment can be spacing at the pencil slot with the aviation plug pencil to support through first support holder, thereby can effectively avoid not hard up of aviation plug.
Other features of the present invention and advantages thereof will become apparent from the following detailed description of exemplary embodiments of the invention, which proceeds with reference to the accompanying drawings.
Drawings
The accompanying drawings, which are incorporated in and constitute a part of the specification, illustrate embodiments of the invention and together with the description, serve to explain the principles of the invention.
Figure 1 is an exploded view of an embodiment of an aviation plug harness retention mechanism of the present disclosure.
The figures are labeled as follows:
the wire harness support comprises a main support-1, a wire harness slot-11, a first support fixing part-12, a first support fixing hole-120, a first support-2, a first support section-21, a wire binding hole-210, a first connecting section-22, a closed support-3, a second support-4, a second support section-41 and a second connecting section-42.
Detailed Description
Various exemplary embodiments of the present invention will now be described in detail with reference to the accompanying drawings. It should be noted that: unless specifically stated otherwise, the relative arrangement of the components and steps, the numerical expressions, and numerical values set forth in these embodiments do not limit the scope of the present invention.
The following description of at least one exemplary embodiment is merely illustrative in nature and is in no way intended to limit the invention, its application, or uses.
Techniques, methods, and apparatus known to those of ordinary skill in the relevant art may not be discussed in detail but are intended to be part of the specification where appropriate.
In all examples shown and discussed herein, any particular value should be construed as merely illustrative, and not limiting. Thus, other examples of the exemplary embodiments may have different values.
It should be noted that: like reference numbers and letters refer to like items in the following figures, and thus, once an item is defined in one figure, further discussion thereof is not required in subsequent figures.
As shown in fig. 1, the aviation plug wire harness fixing mechanism of the present disclosure includes a main bracket 1, a first support bracket 2, and a closing bracket 3.
The main stand 1 is provided with a plurality of wire harness slots 11. The plurality of harness slots 11 each extend in the width direction of the main stand 1, and the harness slots 11 have an open end and a closed end. The harness slot 11 may be used to retain an aircraft plug harness on the primary support 1. A first support bracket fixing part 12 is provided on the baffle between two adjacent wire harness slots 11.
The first support stent 2 comprises a first support section 21 and a first connection section 22. The first support section 21 and the first connecting section 22 have an included angle therebetween. The first support section 21 may be used to support an aviation plug wiring harness. The first connecting section 22 can be used to connect with the first support stent anchoring portion 12. The first connecting section 22 and the first support bracket fixing portion 12 can be connected together by welding, bolting, or snapping.
The closing bracket 3 may be adapted to be detachably connected to the main bracket 1 to close the open end after the aircraft plug wire harness enters the harness slot 11 from the open end.
When the aviation plug wiring harness fixing mechanism is used, the first support bracket 2 is firstly installed on the main bracket 1, and then an aviation plug wiring harness is moved into the wiring harness slot 11 from the opening end of the wiring harness slot 11. After the aviation plug wire harnesses all enter the wire harness slot 11, the closed bracket 2 is adopted to close the opening end of the wire harness slot 11 so as to reliably fix the aviation plug wire harnesses in the aviation plug wire harness fixing mechanism.
The aviation plug wire harness fixing mechanism can limit the aviation plug wire harness in the wire harness slot 11 and support the aviation plug wire harness through the first supporting bracket 2, so that looseness of the aviation plug can be effectively avoided.
In one embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, to better avoid the aviation plug wire harness fixing mechanism from shaking, a plurality of wire harness slots 11 are arranged in parallel.
In one embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, in order to better avoid the aviation plug wire harness fixing mechanism from wobbling, the depth of the wire harness slot 11 is greater than or equal to 80% of the width of the main bracket 1.
In one embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, in order to better avoid wobbling of the aviation plug wire harness fixing mechanism, the main bracket 1 has a plate-like shape, and the wire harness slot 11 covers an area of less than or equal to 40% of the surface area of the main bracket 1.
In one embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, in order to more conveniently and reliably mount the first support bracket 2 to the main bracket 1, the first support bracket fixing portion 12 is provided with a first support bracket fixing hole 120. The first support bracket 2 can be coupled with the first support bracket fixing portion 12 through the first support bracket fixing hole 120 and the fixing hole provided on the first coupling section 22.
In one embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, in order to better avoid the aviation plug wire harness from shaking, the first supporting section 21 and the first connecting section 22 have an included angle of 90 °.
In an embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, in order to better avoid the aviation plug wire harness from shaking, the first support section 21 is provided with a plurality of wire binding holes 210. The aviation plug wire harness can be fixed on the first support bracket 2 through the wire binding holes 210.
In one embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, the closing bracket 3 is bolted to the main bracket 1, thereby more reliably closing the open end of the wire harness slot 11.
In an embodiment of the aviation plug wire harness fixing mechanism of the present disclosure, in order to better avoid the aviation plug wire harness fixing mechanism from shaking, the aviation plug wire harness fixing mechanism further includes a second support bracket 4.
The second support bracket 4 includes a second support section 41 and a second connection section 42. The second support section 41 and the second connection section 42 have an included angle therebetween of 90 ° or more. The second connecting section 42 is fixedly connected to the side of the main stand 1 provided with the closed end of the wire harness slot 11, and the fixed connection may be achieved by welding, bolting, or the like. The second support section 41 may be in contact with a placement plane of the aviation plug harness attachment mechanism to support the aviation plug harness attachment mechanism on the placement plane.
When the aviation plug wire harness fixing mechanism rocks, the second supporting bracket 4 can rock and transmit to the placing plane of the aviation plug wire harness fixing mechanism, so that the aim of avoiding the aviation plug wire harness fixing mechanism from rocking is fulfilled.
The utility model also provides an aviation plug fixed subassembly, including aviation plug, socket and the aviation plug pencil fixed establishment of this disclosure. The distance between the main bracket 1 and the socket is more than or equal to 150mm and less than or equal to 300mm, so that the aviation plug wire harness is better prevented from shaking.
Although certain specific embodiments of the present invention have been described in detail by way of example, it should be understood by those skilled in the art that the foregoing examples are for purposes of illustration only and are not intended to limit the scope of the invention. It will be appreciated by those skilled in the art that modifications may be made to the above embodiments without departing from the scope and spirit of the invention. The scope of the invention is defined by the appended claims.
Claims (10)
1. An aviation plug wire harness fixing mechanism is characterized by comprising a main support, a first support and a closed support; wherein,
the wire harness support is characterized in that a plurality of wire harness slots are formed in the main support, the wire harness slots extend along the width direction of the main support, each wire harness slot is provided with an opening end and a closed end, and a first support fixing part is arranged on a baffle plate between every two adjacent wire harness slots;
the first support bracket comprises a first support section and a first connecting section, an included angle is formed between the first support section and the first connecting section, the first support section is used for supporting the aviation plug wiring harness, and the first connecting section is used for being connected with the first support bracket fixing part;
the closing bracket is configured for detachable connection with the main bracket to close the open end after an aircraft plug harness enters the harness slot from the open end.
2. The aviation plug wire harness retention mechanism according to claim 1, wherein a plurality of said wire harness slots are arranged in parallel.
3. The aviation plug wire harness retention mechanism of claim 1, wherein the wire harness slot has a depth greater than or equal to 80% of the width of the primary bracket.
4. The aviation plug wire harness retention mechanism according to claim 1, wherein said primary bracket has a plate-like shape, said wire harness slot coverage area being less than or equal to 40% of a surface area of said primary bracket.
5. The aviation plug wire harness securing mechanism according to claim 1, wherein the first support bracket securing portion is provided with a first support bracket securing hole.
6. The aviation plug wire harness retention mechanism of claim 1, wherein the first support section and the first connector section define a 90 ° angle therebetween.
7. The aviation plug wire harness securing mechanism according to claim 1, wherein the first support section is provided with a plurality of wire binding holes.
8. The aviation plug wire harness attachment mechanism of claim 1, wherein the closure bracket is bolted to the main bracket.
9. The aviation plug wiring harness retention mechanism of any one of claims 1 to 8, further comprising a second support bracket;
the second supports the support and includes second support section and second linkage segment, the second support section with have between the second linkage segment and be greater than or equal to 90 contained angle, the second linkage segment with the main support is equipped with one side fixed connection of pencil slot the blind end, the second support section set up to with aviation plug pencil fixed establishment's the plane of placing contacts to support aviation plug pencil fixed establishment on placing the plane.
10. An aviation plug securing assembly, comprising an aviation plug, a socket and an aviation plug wire harness securing mechanism as claimed in any one of claims 1 to 9; wherein,
the distance between the main bracket and the socket is greater than or equal to 150mm and less than or equal to 300 mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921175142.6U CN210167746U (en) | 2019-07-24 | 2019-07-24 | Aviation plug wire harness fixing mechanism and aviation plug fixing assembly |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201921175142.6U CN210167746U (en) | 2019-07-24 | 2019-07-24 | Aviation plug wire harness fixing mechanism and aviation plug fixing assembly |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN210167746U true CN210167746U (en) | 2020-03-20 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201921175142.6U Active CN210167746U (en) | 2019-07-24 | 2019-07-24 | Aviation plug wire harness fixing mechanism and aviation plug fixing assembly |
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| Country | Link |
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| CN (1) | CN210167746U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110459995A (en) * | 2019-07-24 | 2019-11-15 | 河南中烟工业有限责任公司 | A kind of aviation plug harness fixed mechanism and aviation plug fixation kit |
-
2019
- 2019-07-24 CN CN201921175142.6U patent/CN210167746U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110459995A (en) * | 2019-07-24 | 2019-11-15 | 河南中烟工业有限责任公司 | A kind of aviation plug harness fixed mechanism and aviation plug fixation kit |
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